Research on Development of Foreign Integral Solid Rocket Ramjet Engine Technology

Missile power plant is a key factor in determining the missile’s range. This paper analyzes and discusses the current patented technologies and application status of integrated solid rocket ramjet engines in foreign countries (USA, Russia, Europe). Based on the analysis, the key technolo...

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Autor principal:	Liu Ying, Lu Ning, Shen Xin
Formato:	article
Lenguaje:	ZH
Publicado:	Editorial Office of Aero Weaponry 2021
Materias:	\|integral solid rocket ramjet engine\|patent\|gas flow\|propellant\|thermal protection\|aerodynamic profile Motor vehicles. Aeronautics. Astronautics TL1-4050
Acceso en línea:	https://doaj.org/article/ad08c68ce9ae48bb88f500b669a80f50
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id	oai:doaj.org-article:ad08c68ce9ae48bb88f500b669a80f50
record_format	dspace
spelling	oai:doaj.org-article:ad08c68ce9ae48bb88f500b669a80f502021-11-30T00:13:23ZResearch on Development of Foreign Integral Solid Rocket Ramjet Engine Technology1673-504810.12132/ISSN.1673-5048.2020.0166https://doaj.org/article/ad08c68ce9ae48bb88f500b669a80f502021-10-01T00:00:00Zhttps://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/1636698882459-476101853.pdfhttps://doaj.org/toc/1673-5048Missile power plant is a key factor in determining the missile’s range. This paper analyzes and discusses the current patented technologies and application status of integrated solid rocket ramjet engines in foreign countries (USA, Russia, Europe). Based on the analysis, the key technologies for the development of integrated solid rocket ramjet are summarized, mainly including gas flow regulation and control, high-energy oxygen poor propellant, thermal strength of structure and long-term thermal protection, wide range adjustable intake and exhaust, integrated aerodynamic shape design of missile and engine, etc.Liu Ying, Lu Ning, Shen XinEditorial Office of Aero Weaponryarticle\|integral solid rocket ramjet engine\|patent\|gas flow\|propellant\|thermal protection\|aerodynamic profileMotor vehicles. Aeronautics. AstronauticsTL1-4050ZHHangkong bingqi, Vol 28, Iss 5, Pp 46-52 (2021)
institution	DOAJ
collection	DOAJ
language	ZH
topic	\|integral solid rocket ramjet engine\|patent\|gas flow\|propellant\|thermal protection\|aerodynamic profile Motor vehicles. Aeronautics. Astronautics TL1-4050
spellingShingle	\|integral solid rocket ramjet engine\|patent\|gas flow\|propellant\|thermal protection\|aerodynamic profile Motor vehicles. Aeronautics. Astronautics TL1-4050 Liu Ying, Lu Ning, Shen Xin Research on Development of Foreign Integral Solid Rocket Ramjet Engine Technology
description	Missile power plant is a key factor in determining the missile’s range. This paper analyzes and discusses the current patented technologies and application status of integrated solid rocket ramjet engines in foreign countries (USA, Russia, Europe). Based on the analysis, the key technologies for the development of integrated solid rocket ramjet are summarized, mainly including gas flow regulation and control, high-energy oxygen poor propellant, thermal strength of structure and long-term thermal protection, wide range adjustable intake and exhaust, integrated aerodynamic shape design of missile and engine, etc.
format	article
author	Liu Ying, Lu Ning, Shen Xin
author_facet	Liu Ying, Lu Ning, Shen Xin
author_sort	Liu Ying, Lu Ning, Shen Xin
title	Research on Development of Foreign Integral Solid Rocket Ramjet Engine Technology
title_short	Research on Development of Foreign Integral Solid Rocket Ramjet Engine Technology
title_full	Research on Development of Foreign Integral Solid Rocket Ramjet Engine Technology
title_fullStr	Research on Development of Foreign Integral Solid Rocket Ramjet Engine Technology
title_full_unstemmed	Research on Development of Foreign Integral Solid Rocket Ramjet Engine Technology
title_sort	research on development of foreign integral solid rocket ramjet engine technology
publisher	Editorial Office of Aero Weaponry
publishDate	2021
url	https://doaj.org/article/ad08c68ce9ae48bb88f500b669a80f50
work_keys_str_mv	AT liuyingluningshenxin researchondevelopmentofforeignintegralsolidrocketramjetenginetechnology
_version_	1718406883530768384

Research on Development of Foreign Integral Solid Rocket Ramjet Engine Technology

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